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(2014 FA44)
Classification: Amor [NEO]          SPK-ID: 3666733
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

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For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.


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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 29 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1889106529548391 2.6312e-05  
a 1.292713216779326 4.7387e-05 au
q 1.048505918914194 4.421e-06 au
i .9764176571495575 0.00011813 deg
node 45.26166696123537 7.4365e-05 deg
peri 190.6992230153296 0.0005283 deg
M 38.65189893169615 0.082848 deg
tp 2458942.860521213240
(2020-Apr-03.36052121)
0.12038 TDB
period 536.8484585945516
1.47
0.029519
8.082e-05
d
yr
n .6705802992197575 3.6872e-05 deg/d
Q 1.536920514644459 5.6339e-05 au
  Orbit Determination Parameters
   # obs. used (total)      105  
   data-arc span      83 days  
   first obs. used      2014-03-29  
   last obs. used      2014-06-20  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .46808  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:41:50  

Additional Information
 Earth MOID = .0370052 au 
 Jupiter MOID = 3.45512 au 
 T_jup = 5.004 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 24.8   n/a E2014M17  
rotation period rot_per 3.5 h n/a LCDB (Rev. 2019-August); Warner et al., 2009 Result based on less than full coverage, so that the period may be wrong by 30 percent or so.
Published Reference List:
[Thirouin, A.; Moskovitz, N.; Binzel, R.P.; Christensen, E.; et al. (2016) Astron. J. 152, A163.]

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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